Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
05002993-2776CA
METHOD AND SYSTEM FOR DETERMINING A THROTTLE POSITION OF AN AIRCRAFT
TECHNICAL FIELD
The present disclosure relates generally to throttles, and, more particularly,
to methods
and systems for determining a throttle position of an aircraft.
BACKGROUND OF THE ART
An electronic engine controller (EEC) may be connected to a throttle lever
used for
controlling operation of an aircraft engine. Prior art systems for determining
aircraft throttle lever
angle (TLA) at an EEC may be suitable for their intended purposes. However,
improvement in
the aerospace industry is always desirable.
SUMMARY
In one aspect, there is provided a method for determining a throttle position
of an
aircraft. The method comprises: obtaining a first throttle position from a
first sensor, a second
throttle position from a second sensor, and a third throttle position from a
third sensor, the first,
second, and third sensors separately coupled to a throttle of the aircraft for
obtaining
independent throttle position measurements therefrom; determining a difference
between the
first throttle position and the second throttle position; detecting a mismatch
when the difference
between the first throttle position and the second throttle position exceeds a
threshold; in
response to detecting the mismatch, selecting a valid one of the first
throttle position and the
second throttle position based on the third throttle position; and outputting
a signal indicative of
the throttle position based on the valid one of the first throttle position
and the second throttle
position.
In one aspect, there is provided an electronic engine controller for
determining a throttle
position of an aircraft. The electronic engine controller comprises at least
one processing unit
and at least one non-transitory memory communicatively coupled to the at least
one processing
unit and comprising computer-readable program instructions. The computer-
readable program
instructions executable by the at least one processing unit for: obtaining a
first throttle position
from a first sensor, a second throttle position from a second sensor, and a
third throttle position
from a third sensor, the first, second, and third sensors separately coupled
to a throttle of the
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aircraft for obtaining independent throttle position measurements therefrom;
determining a
difference between the first throttle position and the second throttle
position; detecting a
mismatch when the difference between the first throttle position and the
second throttle position
exceeds a threshold; in response to detecting the mismatch, selecting a valid
one of the first
throttle position and the second throttle position based on the third throttle
position; and
outputting a signal indicative of the throttle position based on the valid one
of the first throttle
position and the second throttle position.
In one aspect, there is provided a system for determining a throttle position
of an aircraft.
The system comprising: a first sensor, a second sensor and a third sensor
separately coupled to
a throttle for obtaining independent throttle position measurements therefrom;
an electronic
engine controller coupled to the first sensor, the second sensor, and the
third sensor, the
electronic engine controller configured for: obtaining a first throttle
position from the first sensor,
a second throttle position from the second sensor, and a third throttle
position from the third
sensor; determining a difference between the first throttle position and the
second throttle
position; detecting a mismatch when the difference between the first throttle
position and the
second throttle position exceeds a threshold; in response to detecting the
mismatch, selecting a
valid one of the first throttle position and the second throttle position
based on the third throttle
position; and outputting a signal indicative of the throttle position based on
the valid one of the
first throttle position and the second throttle position.
DESCRIPTION OF THE DRAWINGS
Reference is now made to the accompanying figures in which:
Figure 1 is a schematic cross-sectional view of an example gas turbine engine,
in
accordance with one or more embodiments;
Figure 2 is a schematic of an example system for determining a throttle
position, in
accordance with one or more embodiments;
Figure 3 is a schematic of the system of Figure 2 with an electronic engine
controller
having two channels, in accordance with one or more embodiments;
Figure 4 is a flowchart illustrating an example method for determining a
throttle position,
in accordance with one or more embodiments; and
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Figure 5 is an example computing device for implementing a method and/or
system for
determining a throttle position, in accordance with one or more embodiments.
It will be noted that throughout the appended drawings, like features are
identified by like
reference numerals.
DETAILED DESCRIPTION
Figure 1 illustrates a gas turbine engine 10, which may be used with the
systems and
methods for determining a throttle position of an aircraft described herein.
The engine 10
generally comprising in serial flow communication a fan 12 through which
ambient air is
propelled, a compressor section 14 for pressurizing the air, a combustor 16 in
which the
compressed air is mixed with fuel and ignited for generating an annular stream
of hot
combustion gases, and a turbine section 18 for extracting energy from the
combustion gases.
Note that while engine 10 is a turbofan engine, the systems and methods for
determining a
throttle position of an aircraft may be applicable to turboprop engines,
turboshaft engines, or
other suitable types of aircraft engines.
With reference to Figure 2, a system 200 for determining a throttle position
of an aircraft
is illustrated. The system 200 comprises an electronic engine controller (EEC)
210. The system
200 may comprise a plurality of sensors 221, 222, 223 connected to the EEC
210. Alternatively,
the sensors 221, 222, 223 may be separate from the system 200. The EEC 210 is
configured to
obtain a first throttle position from a first sensor 221, a second throttle
position from a second
sensor 222, and a third throttle position from a third sensor 223. The first
sensor 221, the
second sensor 222, and the third sensor 223 are separately coupled to a
throttle 220 of the
aircraft for obtaining independent throttle position measurements therefrom.
The throttle 220
may be provided as part of the system 200 or separate therefrom. The throttle
220 may be
referred to as a throttle quadrant. The EEC 210 is configured to determine a
difference between
the first throttle position and the second throttle position. The EEC 210 is
configured to detect a
mismatch when the difference between the first throttle position and the
second throttle position
exceeds a threshold. The EEC 210 is configured to select a valid one of the
first throttle position
and the second throttle position based on the third throttle position, in
response to detecting the
mismatch. The EEC 210 is configured to output a signal indicative of the
throttle position based
on the valid one of the first throttle position and the second throttle
position. The throttle position
may be referred to as a throttle lever angle (TLA). The throttle position
could be used by the
EEC 210 to control operation of the engine. Accordingly, the signal indicative
of the throttle
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position may be a control signal to the engine 10 and/or one or more
components of the engine
for controlling operation thereof.
The sensors 221, 222, 223 may be any suitable sensors for measuring throttle
position.
While the sensors 221, 222, 223 are illustrated as being internal to the
throttle 220, in some
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embodiment, one or more of the sensors 221, 222, 223 may be provided external
of the throttle
220. One or more of the sensors 221, 222, 223 may be configured for providing
an analog
signal indicative of the measured throttle position. One or more of the
sensors 221, 222, 223
may be configured for providing a digital signal indicative of the measured
throttle position. By
way of a specific and non-limiting example, the first and second sensors 221,
222 may provide
10
analog signals for the first throttle position and the second throttle
position, respectively; and the
third sensor 223 may provide a digital signal for the third throttle position.
By way of another
example, all of the sensors 221, 222, 223 may provide the throttle position
digitally. In some
embodiments, ARI NC 429 communication protocol may be used for transmitting
one or more of
the first, second and third throttle positions digitally. Any other suitable
communication protocol
may be used for transmitting the throttle positions. In some embodiments, one
or more of the
sensors 221, 222, 223 are implemented by a rotary variable differential
transformer (RVDT). In
some embodiments, one or more of the sensors 221, 222, 223 are implemented by
a Hall effect
sensor. By way of a specific and non-limiting example, the first sensor 221
may be a first RVDT,
the second sensor may be a second RVDT, and the third sensor may be a Hall
effect sensor.
By way of another example, the first sensor 221 may be a first RVDT, the
second sensor may
be a second RVDT, and the third sensor may be a third RVDT. Other
configurations for the
sensor types are contemplated.
The first throttle position, the second throttle position and/or the third
throttle position
may be continuously received (e.g., in real time) and/or may be received in
accordance with any
suitable time interval or irregularly. Additionally or alternatively, the
first throttle position, the
second throttle position and/or the third throttle position may be provided by
one or more aircraft
or/and engine computers and/or by any other suitable intermediary device(s).
The aircraft and/or
engine computer and/or intermediary device(s) may be configured for obtaining
the first, second
and/or third throttle position from the sensor(s) 231, 232 and/or 233.
The threshold used for detecting the mismatch may vary depending on practical
implementations. The threshold may be predetermined based on the configuration
of one or
more of the throttle 220, the sensor 221, 222, 223, and/or the EEC 210. The
threshold may be
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stored in memory and/or a storage device and obtained when needed.
Alternatively, the
threshold may be determined when needed.
The selection of the valid one of the first throttle position and the second
throttle position
based on the third throttle position may vary depending on practical
implementations. For
example, a first throttle position difference between first throttle position
and the third throttle
position may be determined. A second throttle position difference between the
second throttle
position and the third throttle position may be determined. The first throttle
position difference
and the second throttle position difference may be compared to each other to
determine which
one of the first throttle position difference and the second throttle position
difference is smaller.
When the first throttle position difference is smaller than the second
throttle position difference,
then the first throttle position is selected as the valid one. When the second
throttle position
difference is smaller than the first throttle position difference, then the
second throttle position is
selected as the valid one.
The signal indicative of the throttle position may correspond to the selected
one of the
first throttle position and the second throttle position. The signal
indicative of the throttle position
may be determined based on the selected one of the first throttle position and
the second
throttle position. The signal indicative of the throttle position may be
determined based on the
third throttle position and the selected one of the first throttle position
and the second throttle
position. For example, an average of the third throttle position and the
selected one of the first
throttle position and the second throttle position may be used to determine
the throttle position.
With additional reference to Figure 3, in some embodiments, the EEC 210
comprises
two channels A, B. In some embodiments, the first channel A obtains the first
throttle position
from the first sensor 221 and the second channel B obtains the second throttle
position from the
second sensor 222. Alternatively, in some embodiments, both the first channel
A and the
second channel B obtain the first throttle position from the first sensor 221
and the second
throttle position from the second sensor 222. In some embodiments, both
channels A, B obtain
the third throttle position from the third sensor 223. Alternatively, one of
the channels (e.g.,
channel A) may obtain the third throttle position and provide the third
throttle position to the
other channel (e.g., channel B). The channels A, B may be in communication
with each other for
providing their obtained throttle position(s). For example, channel A may
provide the first throttle
position to channel B, and channel B may provide the second throttle position
to channel A.
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In some embodiments, one of the channels (e.g., channel A) is selected as
being active, while
the other channel (e.g., channel B) remains inactive. When a channel is
active, that channel is
configured to obtain the first throttle position, the second throttle position
and the third throttle
position. For example, when channel A is active, channel A obtains the first
throttle position from
the first sensor 221, the second throttle position from the second sensor 222
via channel B, and
the third throttle position from the third sensor 223. Similarly, for example,
when channel B is
active, channel B obtains the first throttle position from the first sensor
221 via channel A, the
second throttle position from the second sensor 222, and the third throttle
position from the third
sensor 223. The active channel is further configured to determine the
difference between the
first throttle position and the second throttle position, detect the mismatch
when the difference
exceeds the threshold, and select the valid one of the first throttle position
and the second
throttle position based on the third throttle position, and output the signal
indicative of the throttle
position based on the valid one of the first throttle position and the second
throttle position.
In some embodiments, whether a channel is active or not, all channels may
obtain the
first throttle position, the second throttle position and the third throttle
position, determine the
difference between the first throttle position and the second throttle
position, detect the
mismatch when the difference exceeds the threshold, and select the valid one
of the first throttle
position and the second throttle position based on the third throttle
position. In such cases, the
difference between an active and an inactive channel is that the active
channel outputs the
signal indicative of the throttle position based on the valid one of the first
throttle position and
the second throttle position, while the inactive channel remains passive. In
this manner, the
inactive channel is ready for a transition from inactive to active, such that
said transition will be
seamless.
It should be appreciated that when there is a discrepancy between a first and
second
throttle position (e.g., due to cross channel signal mismatch), that a valid
one of the first and
second throttle position can be determined based on a third throttle position
from a third sensor,
and the valid throttle position may then be used for controlling engine
operation.
The EEC 210 may be interchanged with any other suitable aircraft and/or engine
computer and functionality of the EEC 210 described herein may be implemented
by that
.. computer.
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With reference to Figure 4, there is shown a flowchart illustrating an example
method
400 for determining a throttle position of an aircraft. The method 400 may be
implemented by a
EEC, such as the EEC 210, or may be implemented by any other suitable engine
and/or aircraft
computer. While the method 400 is described herein with reference to the
system 200 of Figure
2 and the engine 10 of Figure 1, this is for example purposes only.
At step 402, a first throttle position, a second throttle position, and a
third throttle position
are obtained. The first throttle position is obtained from a first sensor 221.
The second throttle
position is obtained from a second sensor 222. The third throttle position is
obtained from a third
sensor 223. The first, second, and third sensors 221, 222, 223 are separately
coupled to a
throttle 220 of the aircraft for obtaining independent throttle position
measurements therefrom.
At step 404, a difference between the first throttle position and the second
throttle
position is determined. The first throttle position and the second throttle
position are compared
to each other to determine the difference.
At step 406, a mismatch is detected when the difference between the first
throttle
position and the second throttle position exceeds a threshold. The threshold
may be
predetermined and obtained from memory and/or a storage device during
performance of the
method 400 or may be generated during performance of the method 400 in any
suitable
manner.
At step 408, a valid one of the first throttle position and the second
throttle position is
selected based on the third throttle position. The valid one of the first
throttle position and the
second throttle position may be selected in response to detecting the
mismatch. In some
embodiments, the third throttle position is obtained in response to detecting
the mismatch. In
other words, in some embodiments, the third throttle position may only be
obtained when
needed to determine which one of the first and second throttle position is
valid.
At step 410, a signal indicative of the throttle position based on the valid
one of the first
throttle position measurement and the second throttle position is outputted.
In some
embodiments, the signal indicative of the throttle position corresponds to the
valid one of the
first throttle position and the second throttle position. In some embodiments,
the third throttle
position is used in determining the throttle position for the output signal.
For example, the signal
indicative of the throttle position may correspond to an average of the third
throttle position and
the valid one of the first throttle position and the second throttle position.
Operation of the
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engine 10 may be controlled based on the valid one of the first throttle
position measurement
and the second throttle position measurement.
The method 400 may be performed by an active channel of the EEC 210. The
active
channel may obtain one of the first throttle position from the first sensor
221 and the second
throttle position from the second sensor 222 via the passive channel of the
EEC 210, for
example, as noted above in relation to Figure 3.
In some embodiments, the third throttle position may be used to select one of
the first
throttle position and the second throttle position irrespective of whether or
not a mismatch is
detected. Accordingly, in some embodiments, steps 404 and 406 may be omitted
from the
method 400.
With reference to Figure 5, the system 200 and/or the method 400 may be
implemented
using at least one computing device 500. For example, the EEC 210, may be
implemented by at
least one computing device 500. In some embodiments, each channel A, B of the
EEC 210 is
implemented by at least one computing device 500. The computing device 500
comprises a
processing unit 512 and a memory 514 which has stored therein computer-
executable
instructions 516. The processing unit 512 may comprise any suitable devices
such that
instructions 516, when executed by the computing device 500 or other
programmable
apparatus, may cause at least in part the functions/acts/steps of the method
400 as described
herein to be executed. The processing unit 512 may comprise, for example, any
type of general-
purpose microprocessor or microcontroller, a digital signal processing (DSP)
processor, a
central processing unit (CPU), an integrated circuit, a field programmable
gate array (FPGA), a
reconfigurable processor, other suitably programmed or programmable logic
circuits, or any
combination thereof.
The memory 514 may comprise any suitable known or other machine-readable
storage
medium. The memory 514 may comprise non-transitory computer readable storage
medium, for
example, but not limited to, an electronic, magnetic, optical,
electromagnetic, infrared, or
semiconductor system, apparatus, or device, or any suitable combination of the
foregoing. The
memory 514 may include a suitable combination of any type of computer memory
that is located
either internally or externally to device, for example random-access memory
(RAM), read-only
memory (ROM), compact disc read-only memory (CDROM), electro-optical memory,
magneto-
optical memory, erasable programmable read-only memory (EPROM), and
electrically-erasable
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programmable read-only memory (EEPROM), Ferroelectric RAM (FRAM) or the like.
Memory
514 may comprise any storage means (e.g., devices) suitable for retrievably
storing machine-
readable instructions 516 executable by processing unit 512. In some
embodiments, the
computing device 500 can be implemented as part of a full-authority digital
engine controls
(FADEC) or other similar device, including an EEC, an engine control unit
(ECU), and the like.
In some embodiments, the EEC 210 is implemented by a FADEC.
The methods and systems for determining a throttle position described herein
may be
implemented in a high level procedural or object oriented programming or
scripting language, or
a combination thereof, to communicate with or assist in the operation of a
computer system, for
example the computing device 500. Alternatively, the methods and systems for
determining a
throttle position may be implemented in assembly or machine language. The
language may be
a compiled or interpreted language. Program code for implementing the methods
and systems
for determining a throttle position may be stored on a storage media or a
device, for example a
ROM, a magnetic disk, an optical disc, a flash drive, or any other suitable
storage media or
device. The program code may be readable by a general or special-purpose
programmable
computer for configuring and operating the computer when the storage media or
device is read
by the computer to perform the procedures described herein. Embodiments of the
methods and
systems for determining a throttle position may also be considered to be
implemented by way of
a non-transitory computer-readable storage medium having a computer program
stored
thereon. The computer program may comprise computer-readable instructions
which cause a
computer, or in some embodiments the processing unit 512 of the computing
device 500, to
operate in a specific and predefined manner to perform the functions described
herein.
Computer-executable instructions may be in many forms, including program
modules,
executed by one or more computers or other devices. Generally, program modules
include
routines, programs, objects, components, data structures, etc., that perform
particular tasks or
implement particular abstract data types. Typically the functionality of the
program modules may
be combined or distributed as desired in various embodiments.
The embodiments described in this document provide non-limiting examples of
possible
implementations of the present technology. Upon review of the present
disclosure, a person of
ordinary skill in the art will recognize that changes may be made to the
embodiments described
herein without departing from the scope of the present technology. For
example, the EEC may
be interchanged with any other suitable computing device. By way of another
example, the
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methods and systems described herein may be applied to any suitable engine,
such as, for
example, industrial engines and/or automobile engines. Yet further
modifications could be
implemented by a person of ordinary skill in the art in view of the present
disclosure, which
modifications would be within the scope of the present technology.
Date Recue/Date Received 2020-12-11
